EP1469113A1 - Procédé et installation de fabrication d'une préforme de renfort - Google Patents
Procédé et installation de fabrication d'une préforme de renfort Download PDFInfo
- Publication number
- EP1469113A1 EP1469113A1 EP04356050A EP04356050A EP1469113A1 EP 1469113 A1 EP1469113 A1 EP 1469113A1 EP 04356050 A EP04356050 A EP 04356050A EP 04356050 A EP04356050 A EP 04356050A EP 1469113 A1 EP1469113 A1 EP 1469113A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- reinforcing
- support
- manufacturing
- wire
- binder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000002787 reinforcement Effects 0.000 title claims abstract description 46
- 238000004519 manufacturing process Methods 0.000 title claims description 44
- 238000000034 method Methods 0.000 title claims description 18
- 229920005989 resin Polymers 0.000 claims abstract description 8
- 239000011347 resin Substances 0.000 claims abstract description 8
- 230000003014 reinforcing effect Effects 0.000 claims description 92
- 239000011230 binding agent Substances 0.000 claims description 42
- 238000000151 deposition Methods 0.000 claims description 39
- 238000009434 installation Methods 0.000 claims description 27
- 238000003825 pressing Methods 0.000 claims description 26
- 239000000843 powder Substances 0.000 claims description 18
- 229920001169 thermoplastic Polymers 0.000 claims description 16
- 239000004416 thermosoftening plastic Substances 0.000 claims description 16
- 238000010438 heat treatment Methods 0.000 claims description 11
- 230000008021 deposition Effects 0.000 claims description 10
- 239000002131 composite material Substances 0.000 claims description 7
- 230000004913 activation Effects 0.000 claims description 6
- 238000011144 upstream manufacturing Methods 0.000 claims description 6
- 238000003860 storage Methods 0.000 claims description 5
- 239000012943 hotmelt Substances 0.000 claims description 4
- 230000003213 activating effect Effects 0.000 claims description 3
- 239000004840 adhesive resin Substances 0.000 claims description 2
- 229920006223 adhesive resin Polymers 0.000 claims description 2
- 239000000839 emulsion Substances 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 abstract description 3
- 239000002657 fibrous material Substances 0.000 abstract description 2
- 239000004831 Hot glue Substances 0.000 abstract 1
- 238000001746 injection moulding Methods 0.000 abstract 1
- 238000013519 translation Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229920001187 thermosetting polymer Polymers 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- 239000004952 Polyamide Substances 0.000 description 2
- 239000004695 Polyether sulfone Substances 0.000 description 2
- 239000004697 Polyetherimide Substances 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 229920002647 polyamide Polymers 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 229920006393 polyether sulfone Polymers 0.000 description 2
- 229920001601 polyetherimide Polymers 0.000 description 2
- 229920000098 polyolefin Polymers 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004696 Poly ether ether ketone Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- JUPQTSLXMOCDHR-UHFFFAOYSA-N benzene-1,4-diol;bis(4-fluorophenyl)methanone Chemical compound OC1=CC=C(O)C=C1.C1=CC(F)=CC=C1C(=O)C1=CC=C(F)C=C1 JUPQTSLXMOCDHR-UHFFFAOYSA-N 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000011837 pasties Nutrition 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920002530 polyetherether ketone Polymers 0.000 description 1
- 239000004848 polyfunctional curative Substances 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
- B29C64/118—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/30—Auxiliary operations or equipment
- B29C64/307—Handling of material to be used in additive manufacturing
- B29C64/321—Feeding
- B29C64/336—Feeding of two or more materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
- B29C70/384—Fiber placement heads, e.g. component parts, details or accessories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
Definitions
- the present invention relates to the technical field of the manufacture of multi-directional fibrous preforms or reinforcements for the manufacture of parts in composite materials.
- Application FR 2 581 379 has thus proposed making preforms for frustoconical or ellipsoidal parts of revolution, such as jet nozzles, by winding, on a support having pins, a reinforcing thread pre-impregnated with a bonding agent, intended to prevent any relative sliding of the thread on the support, in order to maintain a perfect homogeneity of the distribution of the reinforcement at the level of the fibrous reinforcement.
- Such a manufacturing method allows the production of fibrous reinforcements multidirectional, said winding, having a generally symmetrical shape of revolution.
- this manufacturing process has the disadvantage of not allow the fabrication of multi-directional fibrous reinforcements with complex or left, without axis of symmetry of revolution privileged or, still, with locally concave regions, given the general shape of the reinforcement fibrous.
- the process according to the application FR 2581 379 has the drawback to place the reinforcing thread, as and when it is removed, in a state that could be called prestressed.
- this prestress influences the behavior mechanical fiber reinforcement multidirectional and can affect the performance of the part incorporating this fibrous reinforcement.
- the winding of the reinforcing wire imposes, because of the applied voltage to the latter, a trajectory of removal necessarily corresponding to a geodesic of the support surface and thus limits the types of reinforcement structures achievable.
- the invention relates to a method of manufacturing a multidirectional fibrous reinforcement, intended to constitute a porous preform for producing a composite material part, a method of depositing at least one reinforcing thread in successive layers on a support, in association with a binder, so as to ensure, on the one hand, adhesion of the first layer on the surface of the support and, secondly, a connection of the successive layers together.
- this manufacturing method is characterized in that it consists in addition, when removing the reinforcing thread, pressing this reinforcing thread against the support or a previous layer by exerting a substantially directional pressure perpendicular to the surface of the support at the point of removal of the wire and thus ensure, thanks to the binder, keeping the thread on its point of deposit, and as and when his removal.
- the binding of the reinforcing thread, at its point of delivery, with the support or the son of the layer on which it is deposited, is done through the binder by application pressure in particular.
- activation of the binder is necessary, for the latter to assume its function of maintaining the wire of reinforcement at its drop point.
- the binder is deposited as and when measurement, upstream of the reinforcement wire in a liquid or pasty state in which it is able to assume its link function and no additional activation is therefore necessary.
- the method according to the invention therefore allows, as and when the removal reinforcing wire and simultaneously or almost simultaneously with the latter, position the wire on a given form, the binder ensuring its maintenance, by adhesion, in this position, to prevent slipping or subsequent movement.
- a binder associated with the pressure exerted on the wire during its removing, allows to position, particularly accurately, the son or son of reinforcement deposited, according to predefined curves that do not correspond necessarily to geodesic lines of the surface of the support. So the process according to the invention allows the formation of preforms on a flat support or, again, the formation of preforms on a conical support, with removal of reinforcing threads circumferentially and according to generators of the surface.
- the manufacturing method according to the invention can be implemented for various other forms of supports.
- This advantageous characteristic of the invention allows the realization of a multidirectional fibrous reinforcement that could be considered to have a isotropic behavior or, at the very least, not having a direction resistance induced by the tension of the wire, insofar as, according to this characteristic of the invention, the deposited reinforcing threads are free from any prestressing.
- the binder used is activated as and when measuring the removal of the reinforcing wire.
- the binder will then be previously deposited, either on the support or on the reinforcing wire itself.
- the binder is, on the contrary, deposited as the reinforcement wire is removed and upstream of the point of delivery of this latest.
- the reinforcing thread can be deposited in any appropriate way, manually or, again, by means of a PLC.
- the reinforcing thread is deposited by means of a robot or robot equipped with a dispensing finger having a pressing head for exerting pressure on the reinforcing thread and a wire guiding groove up to the pressing head.
- the surface of the pressing head is preferably kept tangent to the surface of the support during the removal of the reinforcement.
- thermoplastic powder it is used, as binder, a thermoplastic powder or a thermosetting powder or, alternatively, a mix of both.
- thermoplastic powders it is possible to mention as non-limiting examples the polyolefin, polyamide, polyethersulfone, while among thermosetting powders it is possible to mention epoxy resin powders with or without hardener, powders phenolic, polyester powders.
- the method then provides for ensuring a heating the area of application of the reinforcement wire, and thus to achieve a thermocompressage. This heating can be achieved, either at the finger deposit by a heating resistor, either by means of a radiating source of heat directed to the area where the reinforcement wire is to be removed.
- the implementation of the above powder can be carried out different ways.
- the powder is previously associated with the reinforcing thread that it overlaps in part at least, or, on the contrary, that powder is projected on the support surface or on the previous layers of reinforcing threads, when removing reinforcement thread.
- thermoplastic powder and / or thermosetting.
- This hot melt resin is then deposited on the support, then on the previous layers of threads, as and when the reinforcing thread and upstream of the removal of the reinforcing thread.
- thermoplastic yarn can be of any suitable nature and, for example but not exclusively, include a polyamide, polyolefin, polyethersulfone, polyetheretheracetone (PEEK) or polyetherimide (PEI).
- a binder is used, intimately bonded to the reinforcing wire to form a hybrid reinforcing wire. So, he is It is possible to use thermoplastic filaments as binder same nature as the thermoplastic yarns above, which will be mixed with filaments of reinforcing material, which mixture will be spun to form a reinforcing thread hybrid.
- a solution or a sprayable emulsion of at least one adhesive resin such as that, for example but not exclusively, a polyacrylic, polyvinyl resin or polyurethane.
- the reinforcing thread can be deposited continuously or, at contrary, in discontinuous segments.
- a pressure between 0.01 bar and 30 bar and preferably between 0.1 bar and 1 bar.
- the point of removal of the reinforcing wire will be heated to a temperature of between 50 ° C and 450 ° C and preferably between 50 ° C and 150 ° C.
- the manufacturing method according to the invention can implement different types of reinforcing threads, such as, for example but not exclusively, carbon, glass, polyesters, aramids, metal or mixtures thereof of these materials.
- reinforcing wire must be understood in the broad sense and includes, for for example, bundles or strands of wires, as well as braids son.
- the invention also relates to a preform comprising several layers reinforcing threads arranged in at least two directions and joined together binder, characterized in that they are manufactured according to the process according to the invention.
- the reinforcing threads constituting the porous preform are in a state rest without being prestressed.
- the removal means can be made in any appropriate way and, according to a preferred form, but not strictly necessary, the means of removal comprise at least one deposit finger having a pressing head intended to exert pressure on the reinforcing wire against the support and a groove of guiding the wire to the pressing head.
- the installation includes means of bringing or advancing the reinforcing thread as it is removed, so as not to induce any tension in the reinforcement thread.
- the installation comprises, in addition, means for applying a binder.
- the latter may furthermore comprise means for activating the binder can be made in any suitable way.
- the activation means comprise means for heating the dispensing and pressure zone of the wire of reinforcement. These heating means can then be made in different ways, such as, for example, in the form of a heating resistor incorporated in the finger or, in the form of a radiating source, such as for example, a source of infrared rays.
- the activation means consist of a source of ultraviolet rays.
- Fig. 1 is a general view of an installation of an exemplary embodiment of an installation for the implementation of the manufacturing process in accordance with the invention.
- Fig. 2 is a detailed view of means for depositing a reinforcing wire equipping the installation illustrated in FIG. 1.
- Fig. 3 is a view similar to FIG. 2, showing the depositing means bearing on a convex surface.
- Figs. 4 to 6 are views of different phases of manufacture of a multidirectional fibrous reinforcement or preform according to the method according to the invention.
- Fig. 7 illustrates an alternative embodiment of removal means capable of equipping an installation for the implementation of the manufacturing method according to the invention.
- the aim of the invention is to enable the manufacture of a fibrous reinforcement multidirectional, likely to have a left three-dimensional shape or complex and intended to constitute a porous preform for the production of a part composite material, for example by injection of a resin into the preform porous, previously arranged in a mold.
- the invention aims to offer a great freedom of form for the realization of multidirectional fibrous reinforcement, to allow a wide variety of applications.
- the invention proposes to use an installation, as illustrated in FIG. 1 and designated as a whole by the reference 1 , allowing an automatic or semi-automatic implementation of the method according to the invention.
- the installation 1 comprises a support 2 whose support surface 3 may be considered as a male or female imprint depending on the application face of the reinforcing wire.
- the support 2 is carried by a table 4 , capable of being displaced in translation in a horizontal plane, along two orthogonal axes X and Y , and in rotation R always in the horizontal plane around a vertical axis.
- the installation 1 also comprises at least one and, according to the example illustrated, exactly one depositing head 5 .
- the depositing head 5 is carried by a gantry 6 , provided with a path of movement 7 , along which the head 5 can be moved in translation.
- the gantry 6 is further supported by a column 8 along which it is capable of moving in vertical translation in the Z direction.
- the table 4 , the gantry 6 and the column 8 are equipped with appropriate automation and motorization means constituting means for moving the deposition head 5 relative to the surface 3 of the support 2 .
- the depositing head 5 then comprises depositing means 10, more particularly illustrated in FIG. 2.
- the depositing means 10 consist of a deposit finger 11 , having, at its end, a pressing head 13 whose surface is intended, as will subsequently appear, to press the reinforcing thread F against the surface 3 of the support 2 .
- the finger has, in addition, a groove 13 1 for guiding the wire to the pressing head 13 .
- the dispensing head has, of course, means for guiding the reinforcing thread F to the finger 11 which can be made in any appropriate manner, such as by grooves or tubes 14 in which the reinforcing thread F passes.
- the deposit finger 11 is rotatable relative to the head 5 , about an axis ⁇ being moved in rotation about this axis by unrepresented motor means.
- the finger 11 is movable in translation relative to the head 5 along the axis ⁇ , being actuated by means, not shown, for modulating the pressing pressure of the pressing head 13 on the surface 3 .
- the installation 1 further comprises storage means 15 for reinforcing wire F which can be made in any suitable manner, such as, for example, in the form of a reel, not shown.
- the installation 1 also comprises means 16 for guiding the reinforcing thread from the storage means 15 to the deposition head 5 .
- the guiding means 16 may be made in any suitable manner and, in the example shown, in the form of a flexible sheath, inside which the reinforcing wire F circulates freely.
- the manufacturing facility 1 further comprises means 20 for controlling the means for moving the head 5 , means for moving the finger 11 , as well as means for moving the support 3 .
- the control means 20 are, for example, made in the form of a control unit or a programmable controller adapted to control the installation 1 , so as to ensure a movement of the finger 11 against the surface 3 of the support, so as to deposit the wire F according to the invention.
- control means 20 ensure a displacement of the deposition head 5 relative to the surface of the support 3 , so as to move the deposition means 10 against the support surface 3 , along a predetermined path, by pressing the wire reinforcement F against the surface of the support 3 and maintaining the pressing surface 13 tangential to the support surface 3 , as shown in FIG. 3 , so that the pressure exerted on the wire F has a normal direction to the surface 3 of the support.
- the reinforcing wire F used is a wire, at least in part, covered with a thermoplastic powder and the dispensing finger 11 then comprises a heating resistor 21 which melts the thermoplastic powder as and when measuring the removal of the wire F , so as to adhere the wire F , first on the surface 3 of the support 2 during the first pass, then on the previous wire layer in the following passes.
- the depositing head comprises means 22 for feeding or advancing the reinforcing thread.
- the supply means 22 comprise, for example, a set of drive rollers 23 which pinch the reinforcing wire and which are rotated by motor means, not shown. The rotation of the rollers 23 is then controlled by the control unit 20 , so as to supply the finger 11 with a length of reinforcing thread F substantially corresponding to the length of the path of the finger 11 on the surface 3 , so as to that the reinforcement wire is deposited there without tension.
- the implementation of an installation allows, for example, the production of a preform for the constitution of an aircraft window frame for example.
- the reinforcing son F illustrated in phantom in FIG. 1 , may be deposited in turns of generally ovoid shape in a plane corresponding to the plane of the support during the first pass, then in radial or centrifugal directions for the second pass, then again in turns for the third pass and so then, until you get the thickness and shape you want.
- the depositing means also comprise means 24 for cutting the wire F controlled by the control unit 20 .
- Figs. 4 and 5 illustrate another example of implementation of the method according to the invention, according to which the preform to be produced must have a cylindrical body 30 with a shoulder 31 .
- the installation and the method according to the invention make it possible to arrange the wire in successive layers in two perpendicular orientations, as is apparent from FIGS. 3 and 5 .
- the method and the installation according to the invention make it possible to ensure the removal of a reinforcing wire along a path of deposition, contained in a radial plane, in the reentrant angle 32 .
- Fig. 6 illustrates an example of trajectory for the simultaneous deposition of two reinforcing son in parallel.
- the dispensing head can be equipped with various accessories.
- FIG. 7 illustrates another embodiment according to which the finger 11 is deposited with, on the one hand, means 35 for applying a binder, such as, for example, a spray nozzle and, on the other hand, activation means 36 which are, in the present case, constituted by a source of ultraviolet rays.
- a binder such as, for example, a spray nozzle
- activation means 36 which are, in the present case, constituted by a source of ultraviolet rays.
- the application means 35 are constituted by a nozzle for depositing a hot melt resin upstream of the wire of reinforcement, as and when the removal of the latter.
- the installation according to the invention could be made of a any other way and, for example, implement an automaton or robot arm articulated.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Robotics (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Optics & Photonics (AREA)
- Moulding By Coating Moulds (AREA)
- Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
- Nonwoven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
- un support dont la surface présente la forme du renfort fibreux à fabriquer,
- des moyens de stockage d'au moins un fil de renfort,
- au moins une tête de dépose qui comprend des moyens de guidage du fil de renfort jusqu'à des moyens de dépose présentant une surface de pressage du fil de renfort contre la surface du support,
- des moyens de guidage du fil de renfort depuis les moyens de stockage jusqu'à la tête de dépose,
- des moyens de déplacement de la tête de dépose,
- des moyens de commande des moyens de déplacement adaptés pour assurer un déplacement de la tête de dépose par rapport à la surface du support, de manière à déplacer les moyens de dépose contre la surface du support selon une trajectoire prédéterminée, en pressant le fil de renfort contre la surface du support et en maintenant la surface de pressage tangente à la surface du support pour que la pression exercée possède une direction normale à la surface du support.
Claims (27)
- Procédé de fabrication d'un renfort fibreux multidirectionnel, destiné à constituer une préforme poreuse pour la réalisation d'une pièce en matériau composite, procédé consistant à déposer au moins un fil de renfort (F) en couches successives sur un support (2), en association avec un liant, de manière à assurer, d'une part, une adhérence de la première couche sur la surface (3) du support (2) et, d'autre part, une liaison des couches successives entre elles,
caractérisé en ce qu'il consiste, en outre, lors de la dépose du fil de renfort, à presser ce fil de renfort (F) contre le support (2) en exerçant une pression de direction sensiblement perpendiculaire à la surface (3) du support (2) au point de dépose du fil (F). - Procédé de fabrication selon la revendication 1, caractérisé en ce qu'il consiste, en outre, à assurer l'avancement du fil de renfort (F) au fur et à mesure de la dépose du fil de renfort, de manière à n'induire aucune tension dans ledit fil de renfort et à le déposer à l'état de repos.
- Procédé de fabrication selon la revendication 1 ou 2, caractérisé en ce qu'il consiste à activer le liant au fur et à mesure de la dépose du fil de renfort (F).
- Procédé selon la revendication 1 ou 2, caractérisé en ce qu'il consiste à déposer le liant en amont du fil de renfort (F) lors de la dépose de ce dernier.
- Procédé de fabrication selon l'une des revendications 1 à 4, caractérisé en ce qu'il consiste à déposer le fil de renfort (F) au moyen d'un doigt de dépose (11) présentant une tête de pressage (13) destinée à exercer une pression sur le fil de renfort et une gorge de guidage du fil (F) jusqu'à la tête de pressage (13).
- Procédé de fabrication selon la revendication 5, caractérisé en ce qu'il consiste à exercer, sur le doigt de dépose (11), une pression perpendiculaire à la surface de la tête de pressage (13) et à maintenir la surface de la tête de pressage (13) tangente à la surface (3) du support (2) pendant la dépose du fil de renfort (F).
- Procédé de fabrication selon la revendication 5, caractérisé en ce qu'il consiste à déposer, simultanément, plusieurs fils de renfort (F) selon des trajectoires de dépose parallèles.
- Procédé de fabrication selon l'une des revendications 1 à 7, caractérisé en ce qu'il consiste à mettre en oeuvre, en tant que liant, une poudre thermoplastique et à chauffer la zone de dépose du fil de renfort.
- Procédé de fabrication selon la revendication 8, caractérisé en ce qu'il consiste à mettre en oeuvre un fil de renfort (F) recouvert, en partie au moins, d'une poudre thermoplastique.
- Procédé de fabrication selon la revendication 8 ou 9, caractérisé en ce qu'il consiste à projeter de la poudre thermoplastique sur la surface lors de la dépose du fil de renfort.
- Procédé de fabrication selon l'une des revendications 8 à 10, caractérisé en ce qu'il consiste à mettre en oeuvre une surface (3) de support (2) recouverte, en partie au moins, d'une poudre thermoplastique.
- Procédé de fabrication selon l'une des revendications 1 à 7, caractérisé en ce qu'il consiste à mettre en oeuvre, en tant que liant, une résine hot melt déposée sur le support au fur et à mesure de la dépose du fil de renfort et en amont de la dépose du fil de renfort.
- Procédé de fabrication selon l'une des revendications 1 à 7, caractérisé en ce qu'il consiste à mettre en oeuvre, en tant que liant, un fil thermoplastique guipé sur le fil de renfort et à chauffer le fil de renfort au niveau de son point de dépose.
- Procédé de fabrication selon l'une des revendications 1 à 7, caractérisé en ce qu'il consiste à mettre en oeuvre, en tant que liant, une solution ou une émulsion pulvérisable d'au moins une résine adhésive.
- Procédé de fabrication selon l'une des revendications 1 à 7, caractérisé en ce qu'il consiste à mettre en oeuvre un liant intimement lié au fil de renfort pour former un fil de renfort hybride.
- Procédé de fabrication selon l'une des revendications 1 à 15, caractérisé en ce qu'il consiste à déposer le fil de renfort en segments discontinus.
- Procédé selon l'une des revendications 1 à 15, caractérisé en ce qu'il consiste :à mettre en oeuvre un support (2) présentant une forme concave localement,à déposer les fils de renfort dans la région concave au moins du support (2).
- Procédé de fabrication selon l'une des revendications 1 à 17, caractérisé en ce qu'il consiste à exercer, sur le fil de renfort (F), une pression comprise entre 0,01 bar et 30 bar et, de préférence, comprise entre 0,1 bar et 1 bar.
- Procédé de fabrication selon l'une des revendications 1 à 18, caractérisé en ce qu'il consiste à chauffer le point de dépose du fil de renfort à une température comprise entre 50 °C et 450 °C et, de préférence, comprise entre 50 °C et 150 °C.
- Préforme poreuse comprenant plusieurs couches de fils de renfort (F) disposées selon au moins deux directions et solidarisées entre elles par un liant, caractérisée en ce qu'elle est fabriquée conformément au procédé de fabrication selon l'une des revendications 1 à 19.
- Préforme poreuse selon la revendication 20, caractérisée en ce que les fils de renfort (F) sont à l'état de repos et ne sont soumis à aucune précontrainte.
- Installation pour la mise en oeuvre du procédé de fabrication selon l'une des revendications 1 à 19, caractérisée en ce qu'elle comprend :un support (2) dont la surface (3) présente la forme du renfort fibreux à fabriquer,des moyens de stockage (15) d'au moins un fil de renfort (F),au moins une tête de dépose (5) qui comprend des moyens de guidage du fil de renfort jusqu'à des moyens de dépose (10) présentant une surface de pressage (13) du fil de renfort contre la surface (3) du support (2),des moyens de guidage (16) du fil de renfort (F) depuis les moyens de stockage (15) jusqu'à la tête de dépose (5),des moyens de déplacement de la tête de dépose (5),des moyens de commande (20) des moyens de déplacement adaptés pour assurer un déplacement de la tête de dépose (5) par rapport à la surface (3) du support (2), de manière à déplacer les moyens de dépose (10) contre la surface (3) du support (2) selon une trajectoire prédéterminée, en pressant le fil de renfort (F) contre la surface (3) du support (2) et en maintenant la surface de pressage (13) tangente à la surface (3) du support (2) pour que la pression exercée possède une direction normale à la surface (3) du support (2).
- Installation selon la revendication 22, caractérisée en ce qu'elle comprend, en tant que moyens de dépose, un doigt de dépose (11) présentant une tête de pressage (13) destinée à exercer une pression sur le fil de renfort contre le support et une gorge de guidage du fil jusqu'à la tête de pressage (13).
- Installation selon la revendication 22 ou 23, caractérisée en ce qu'elle comprend des moyens (22) d'amenée du fil de renfort (F) au fur et à mesure de sa dépose, de manière à n'induire aucune tension dans le fil de renfort (F).
- Installation selon l'une des revendications 22 à 24, caractérisée en ce qu'elle comprend des moyens (35) d'application d'un liant.
- Installation selon l'une des revendications 22 à 25, caractérisée en ce qu'elle comprend des moyens (36) d'activation d'un liant.
- Installation selon la revendication 26, caractérisée en ce que les moyens d'activation (36) comprennent des moyens de chauffage (21) de la zone de dépose et de pression du fil de renfort (F).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0304805A FR2853914B1 (fr) | 2003-04-17 | 2003-04-17 | Procede et installation de fabrication d'une preforme de renfort |
FR0304805 | 2003-04-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1469113A1 true EP1469113A1 (fr) | 2004-10-20 |
EP1469113B1 EP1469113B1 (fr) | 2007-08-22 |
Family
ID=32893381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04356050A Expired - Lifetime EP1469113B1 (fr) | 2003-04-17 | 2004-04-15 | Procédé et installation de fabrication d'une préforme de renfort |
Country Status (7)
Country | Link |
---|---|
US (1) | US7115180B2 (fr) |
EP (1) | EP1469113B1 (fr) |
JP (1) | JP4708725B2 (fr) |
AT (1) | ATE371048T1 (fr) |
DE (1) | DE602004008366T2 (fr) |
ES (1) | ES2293189T3 (fr) |
FR (1) | FR2853914B1 (fr) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2917330A1 (fr) * | 2007-06-12 | 2008-12-19 | Hexcel Reinforcements Soc Par | Procede de fabrication d'un materiau composite dans lequel au moins un fil torsade est depose. |
WO2008155504A3 (fr) * | 2007-06-12 | 2009-03-05 | Hexcel Reinforcements | Procede de fabrication d ' un materiau composite dans lequel au moins un fil torsade est depose et materiau composite ainsi obtenu |
WO2009156157A1 (fr) * | 2008-06-25 | 2009-12-30 | Zsk Stickmaschinen Gmbh | Dispositif et procédé d’application d’un matériau en forme de bande |
EP2345530A1 (fr) * | 2010-01-15 | 2011-07-20 | KraussMaffei Technologies GmbH | Dispositif et procédé destinés à la pulvérisation directe de bandes fibreuses |
WO2012010805A1 (fr) | 2010-07-22 | 2012-01-26 | Hexcel Reinforcements | Nouveau materiau intermediaire de renfort constitue d'un ensemble de fils voiles espaces |
WO2014063944A1 (fr) * | 2012-10-22 | 2014-05-01 | Wobben Properties Gmbh | Procédé et dispositif de fabrication de préformes pour la fabrication d'une pale de rotor |
FR2999973A1 (fr) * | 2012-12-21 | 2014-06-27 | Coriolis Composites | Procede de realisation de preformes a partir de fibres munies d'un liant et machine correspondante |
EP2853382B1 (fr) * | 2004-10-29 | 2020-12-02 | The Boeing Company | Système de superposition de couches de tissu automatisé et procédé |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8632653B2 (en) | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
FR2889104B1 (fr) * | 2005-07-29 | 2009-08-28 | Hexcel Reinforcements Soc Par | Nouveau procede de placement d'au moins un element filaire, particulierement adapte a la constitution de preformes de type annulaire ou ellipsoidale |
ATE418440T1 (de) | 2005-07-29 | 2009-01-15 | Hexcel Reinforcements | Platzierungsverfahren eines drahtelementes, das für die bildung von ring- oder ellipsoidartigen vorformlingen geeignet ist |
BRPI0719134A2 (pt) * | 2006-11-21 | 2014-02-04 | Henkel Corp | Composição de matéria, processos de moldagem por transferência de resina, e de moldagem por transferência de resina assistida por vácuo, pré-forma de moldagem por transferência de resina assistida por vácuo, e, processo de infusão de película de resina |
CN101462316A (zh) * | 2007-12-19 | 2009-06-24 | 维斯塔斯风力系统有限公司 | 预成型件的制备方法 |
CN101462358B (zh) * | 2007-12-19 | 2013-09-11 | 维斯塔斯风力系统有限公司 | 一种制备预成型件的设备 |
US9090028B2 (en) | 2008-04-17 | 2015-07-28 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
EP2565023B1 (fr) * | 2011-08-31 | 2014-05-14 | SSM Schärer Schweiter Mettler AG | dispositif de pose de fils |
US8919410B2 (en) | 2012-03-08 | 2014-12-30 | Fives Machining Systems, Inc. | Small flat composite placement system |
DE102012102841B3 (de) * | 2012-04-02 | 2013-07-11 | Institut Für Verbundwerkstoffe Gmbh | Verfahren zur Präparation eines Roving |
FR3009273B1 (fr) * | 2013-07-30 | 2017-07-28 | Eurocopter France | Cadre en materiaux composites stratifies pour fuselage d'aeronef, comportant des zones de renfort courbes a rayon de courbure evolutif |
DE102016123631A1 (de) | 2016-12-07 | 2018-06-07 | MM Printed Composites GmbH | Vorrichtung und Verfahren zur Erzeugung von dreidimensionalen Objekten sowie dreidimensionales Objekt |
CA3084429A1 (fr) * | 2017-12-06 | 2019-06-13 | Safran Aircraft Engines | Procede de fabrication additive in situ d'un revetement sur un carter de turbomachine |
PL238313B1 (pl) * | 2018-09-14 | 2021-08-09 | Rebuild Spolka Z Ograniczona Odpowiedzialnoscia | Urządzenie do automatycznego zbrojenia konstrukcji i sposób automatycznego zbrojenia konstrukcji |
EP3827967B1 (fr) | 2019-11-26 | 2024-06-12 | Fundación Tecnalia Research & Innovation | Procédé de fabrication additive d'une préforme |
CN114901457A (zh) * | 2020-01-02 | 2022-08-12 | 9T实验室股份公司 | 用于施加细长纤维丝束的设备和方法 |
EP4257321A1 (fr) * | 2022-04-07 | 2023-10-11 | Siemens Gamesa Renewable Energy A/S | Procédé de fabrication d'un élément de construction de préforme et agencement de moule |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0032858A1 (fr) * | 1980-01-17 | 1981-07-29 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Structure tridimensionnelle annulaire |
EP0193380A2 (fr) * | 1985-02-26 | 1986-09-03 | E.I. Du Pont De Nemours And Company | Appareil pour fabriquer une préforme profilée |
FR2581379A1 (fr) * | 1985-05-02 | 1986-11-07 | Europ Propulsion | Procede de fabrication de preforme pour la realisation d'une piece en materiau composite |
WO1998017852A1 (fr) * | 1996-10-18 | 1998-04-30 | E.I. Du Pont De Nemours And Company | Façonnage rapide de tissus |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4410385A (en) * | 1981-01-28 | 1983-10-18 | General Electric Company | Method of making a composite article |
GB2105247B (en) * | 1981-06-23 | 1985-04-24 | Courtaulds Plc | Process for making a fibre-reinforced moulding |
US4735672A (en) * | 1982-05-27 | 1988-04-05 | Lockheed Corporation | Automated fiber lay-up machine |
US4539249A (en) * | 1983-09-06 | 1985-09-03 | Textile Products, Incorporated | Method and apparatus for producing blends of resinous, thermoplastic fiber, and laminated structures produced therefrom |
US4750960A (en) * | 1984-09-10 | 1988-06-14 | Rensselaer Polytechnic Institute | Robotic winding system and method |
JPS61202824A (ja) * | 1985-03-06 | 1986-09-08 | Suriibondo:Kk | 立体構造物の製造方法 |
US5213646A (en) * | 1988-12-28 | 1993-05-25 | Andrew M. Zsolnay | Precision method for placing filaments |
US5296064A (en) * | 1989-04-17 | 1994-03-22 | Georgia Tech Research Corp. | Flexible multiply towpreg tape from powder fusion coated towpreg and method for production thereof |
JP2996495B2 (ja) * | 1990-08-02 | 1999-12-27 | バンドー化学株式会社 | 可撓性袋体繊維成形物の製造方法 |
FR2687389B1 (fr) * | 1992-02-17 | 1994-05-06 | Aerospatiale Ste Nationale Indle | Dispositif et procede pour realiser une piece de structure complexe par depose au contact de fil ou ruban. |
JPH07290475A (ja) * | 1994-04-22 | 1995-11-07 | Asahi Koruku Kogyo Kk | レジンフェルトの製造方法とその装置 |
US5447586A (en) * | 1994-07-12 | 1995-09-05 | E. I. Du Pont De Nemours And Company | Control of thermoplastic tow placement |
DE19957906A1 (de) * | 1999-12-01 | 2001-06-28 | Schunk Kohlenstofftechnik Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauteils sowie Vorrichtung zur Herstellung eines solchen |
US20030196743A1 (en) * | 2002-04-17 | 2003-10-23 | Vincent Borbone | Apparatus and methods for producing tow based patterns |
-
2003
- 2003-04-17 FR FR0304805A patent/FR2853914B1/fr not_active Expired - Fee Related
-
2004
- 2004-04-07 US US10/820,573 patent/US7115180B2/en not_active Expired - Lifetime
- 2004-04-15 AT AT04356050T patent/ATE371048T1/de active
- 2004-04-15 EP EP04356050A patent/EP1469113B1/fr not_active Expired - Lifetime
- 2004-04-15 DE DE602004008366T patent/DE602004008366T2/de not_active Expired - Lifetime
- 2004-04-15 ES ES04356050T patent/ES2293189T3/es not_active Expired - Lifetime
- 2004-04-19 JP JP2004123052A patent/JP4708725B2/ja not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0032858A1 (fr) * | 1980-01-17 | 1981-07-29 | SOCIETE EUROPEENNE DE PROPULSION (S.E.P.) Société Anonyme dite: | Structure tridimensionnelle annulaire |
EP0193380A2 (fr) * | 1985-02-26 | 1986-09-03 | E.I. Du Pont De Nemours And Company | Appareil pour fabriquer une préforme profilée |
FR2581379A1 (fr) * | 1985-05-02 | 1986-11-07 | Europ Propulsion | Procede de fabrication de preforme pour la realisation d'une piece en materiau composite |
WO1998017852A1 (fr) * | 1996-10-18 | 1998-04-30 | E.I. Du Pont De Nemours And Company | Façonnage rapide de tissus |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2853382B1 (fr) * | 2004-10-29 | 2020-12-02 | The Boeing Company | Système de superposition de couches de tissu automatisé et procédé |
FR2917330A1 (fr) * | 2007-06-12 | 2008-12-19 | Hexcel Reinforcements Soc Par | Procede de fabrication d'un materiau composite dans lequel au moins un fil torsade est depose. |
WO2008155504A3 (fr) * | 2007-06-12 | 2009-03-05 | Hexcel Reinforcements | Procede de fabrication d ' un materiau composite dans lequel au moins un fil torsade est depose et materiau composite ainsi obtenu |
US8696850B2 (en) | 2007-06-12 | 2014-04-15 | Hexcel Reinforcements S.A.S. | Method for making a composite material having at least one twisted thread deposited therein |
US9702066B2 (en) | 2007-06-12 | 2017-07-11 | Hexcel Reinforcements, S.A.S. | Composite material having at least one twisted thread deposited therein |
WO2009156157A1 (fr) * | 2008-06-25 | 2009-12-30 | Zsk Stickmaschinen Gmbh | Dispositif et procédé d’application d’un matériau en forme de bande |
EP2345530A1 (fr) * | 2010-01-15 | 2011-07-20 | KraussMaffei Technologies GmbH | Dispositif et procédé destinés à la pulvérisation directe de bandes fibreuses |
US9132606B2 (en) | 2010-07-22 | 2015-09-15 | Hexcel Reinforcements | Intermediate reinforcing material consisting of an array of spaced-apart yarns/webs |
US9796141B2 (en) | 2010-07-22 | 2017-10-24 | Hexcel Reinforcements | Method for making an intermediate reinforcing material consisting of an array of spaced-apart yarns/webs |
WO2012010805A1 (fr) | 2010-07-22 | 2012-01-26 | Hexcel Reinforcements | Nouveau materiau intermediaire de renfort constitue d'un ensemble de fils voiles espaces |
RU2609169C2 (ru) * | 2012-10-22 | 2017-01-30 | Воббен Пропертиз Гмбх | Способ и устройство для изготовления заготовок для изготовления лопасти ротора |
WO2014063944A1 (fr) * | 2012-10-22 | 2014-05-01 | Wobben Properties Gmbh | Procédé et dispositif de fabrication de préformes pour la fabrication d'une pale de rotor |
WO2014096562A3 (fr) * | 2012-12-21 | 2014-09-12 | Coriolis Composites | Procédé de réalisation de préformes a partir de fibres munies d'un liant, et machine correspondante |
FR2999973A1 (fr) * | 2012-12-21 | 2014-06-27 | Coriolis Composites | Procede de realisation de preformes a partir de fibres munies d'un liant et machine correspondante |
Also Published As
Publication number | Publication date |
---|---|
ES2293189T3 (es) | 2008-03-16 |
DE602004008366T2 (de) | 2008-05-15 |
JP4708725B2 (ja) | 2011-06-22 |
FR2853914A1 (fr) | 2004-10-22 |
US7115180B2 (en) | 2006-10-03 |
EP1469113B1 (fr) | 2007-08-22 |
US20050067731A1 (en) | 2005-03-31 |
DE602004008366D1 (de) | 2007-10-04 |
JP2004316062A (ja) | 2004-11-11 |
ATE371048T1 (de) | 2007-09-15 |
FR2853914B1 (fr) | 2005-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1469113B1 (fr) | Procédé et installation de fabrication d'une préforme de renfort | |
CA2683606C (fr) | Procede de fabrication d'un materiau composite dans lequel au moins un fil torsade est depose | |
CA2107671C (fr) | Procede de fabrication d'un fil composite et produits composites obtenus a partir dudit fil | |
CA2347147A1 (fr) | Corps de revolution creux et son procede de fabrication | |
EP1301333B1 (fr) | Corps creux composite et son procede de fabrication | |
EP0557140B1 (fr) | Procédé de dépose au contact à chaud de matériau composite fibré à matrice vitreuse et dispositif pour la mise en ouevre du procédé | |
EP0707941B1 (fr) | Procédé et machine pour l'élaboration de tubes en matériau composite à caractéristiques mécaniques et tribologiques élevées, et tubes obtenus par ledit procédé | |
EP1749643B1 (fr) | Procédé de placement d'au moins un élément filaire, particulièrement adapté à la constitution de préformes de type annulaire ou ellipsoïdale | |
EP0402199B1 (fr) | Procédé de fabrication de manchon électro-soudable, dispositif pour la mise en oeuvre de celui-ci et manchons obtenus selon ce procédé | |
EP2616231B1 (fr) | Procede de fabrication d'un ressort de suspension en materiau composite de mise en oeuvre simplifiee | |
EP2199069B1 (fr) | Fabrication de pièces composites complexes | |
WO2015018799A1 (fr) | Rouleau de compactage pour tête de dépose de fils préimprégnés de résine et procédé de réalisation d'un tel rouleau | |
EP3140105A1 (fr) | Procédé et machine pour la réalisation de préformes par application sans compactage de fibres orientées | |
WO2019048744A1 (fr) | Procédé de réalisation de préformés avec application d'un liant sur fibre sèche formée de plusieurs fibres initiales | |
EP1574319B1 (fr) | Procédé d'enroulement d'un ruban composite et son dispositif de mise en oeuvre | |
FR2469137A1 (fr) | Procede et machine pour realiser un article d'habillement tel qu'un gant de protection | |
EP3740372B1 (fr) | Outil de dépôt en 3 dimensions de matière par extrusion | |
WO2004067264A1 (fr) | Procede de depose sur un support de couches fibreuses inclinees | |
FR3141875A1 (fr) | Outillage d’extrusion de filament renforce pour fabrication additive | |
FR3109425A1 (fr) | Procédé de réalisation d’un réservoir de stockage composite | |
FR2989920A1 (fr) | Procede et dispositif de projection pour former un materiau composite |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL HR LT LV MK |
|
17P | Request for examination filed |
Effective date: 20050318 |
|
17Q | First examination report despatched |
Effective date: 20050415 |
|
AKX | Designation fees paid |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR |
|
17Q | First examination report despatched |
Effective date: 20050415 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REF | Corresponds to: |
Ref document number: 602004008366 Country of ref document: DE Date of ref document: 20071004 Kind code of ref document: P |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20071003 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20071122 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2293189 Country of ref document: ES Kind code of ref document: T3 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20071123 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080122 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20071122 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
26N | No opposition filed |
Effective date: 20080526 |
|
BERE | Be: lapsed |
Owner name: HEXCEL REINFORCEMENTS Effective date: 20080430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080430 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080430 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080223 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080415 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20070822 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20190618 Year of fee payment: 18 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 371048 Country of ref document: AT Kind code of ref document: T Effective date: 20200415 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200415 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200415 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20220303 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20220506 Year of fee payment: 19 Ref country code: DE Payment date: 20220302 Year of fee payment: 19 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 602004008366 Country of ref document: DE Representative=s name: CBDL PATENTANWAELTE GBR, DE |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20230309 Year of fee payment: 20 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230516 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 602004008366 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20230415 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230415 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230415 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231103 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20240527 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230416 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230416 |